EP0376259A2 - Kessel mit vermindertem NOx-Ausstoss - Google Patents

Kessel mit vermindertem NOx-Ausstoss Download PDF

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Publication number
EP0376259A2
EP0376259A2 EP19890123973 EP89123973A EP0376259A2 EP 0376259 A2 EP0376259 A2 EP 0376259A2 EP 19890123973 EP19890123973 EP 19890123973 EP 89123973 A EP89123973 A EP 89123973A EP 0376259 A2 EP0376259 A2 EP 0376259A2
Authority
EP
European Patent Office
Prior art keywords
combustion
premixture
burner
furnace
heat transfer
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP19890123973
Other languages
English (en)
French (fr)
Other versions
EP0376259A3 (de
EP0376259B1 (de
Inventor
Hironobu Kobayashi
Shigeru Azuhata
Kiyoshi Narato
Kenichi Sohma
Yasuo Yoshii
Norio Arashi
Shigekazu Nishimoto
Isao Koyama
Toru Inata
Hideo Kikuchi
Tadayoshi Murakami
Masayuki Taniguchi
Hiroshi Miyadera
Fumio Koda
Tatsuzou Enomoto
Kenji Kobayashi
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hitachi Ltd
Mitsubishi Hitachi Power Systems Ltd
Original Assignee
Babcock Hitachi KK
Hitachi Ltd
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Publication date
Priority claimed from JP32584788A external-priority patent/JPH0264302A/ja
Application filed by Babcock Hitachi KK, Hitachi Ltd filed Critical Babcock Hitachi KK
Publication of EP0376259A2 publication Critical patent/EP0376259A2/de
Publication of EP0376259A3 publication Critical patent/EP0376259A3/de
Application granted granted Critical
Publication of EP0376259B1 publication Critical patent/EP0376259B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D23/00—Assemblies of two or more burners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F22—STEAM GENERATION
    • F22B—METHODS OF STEAM GENERATION; STEAM BOILERS
    • F22B21/00—Water-tube boilers of vertical or steeply-inclined type, i.e. the water-tube sets being arranged vertically or substantially vertically
    • F22B21/34—Water-tube boilers of vertical or steeply-inclined type, i.e. the water-tube sets being arranged vertically or substantially vertically built-up from water tubes grouped in panel form surrounding the combustion chamber, i.e. radiation boilers
    • F22B21/346—Horizontal radiation boilers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F22—STEAM GENERATION
    • F22B—METHODS OF STEAM GENERATION; STEAM BOILERS
    • F22B31/00—Modifications of boiler construction, or of tube systems, dependent on installation of combustion apparatus; Arrangements of dispositions of combustion apparatus

Definitions

  • This invention relates to a boiler which uses a gaseous fuel and more particularly to a boiler suitable for reducing the concentration of nitrogen oxides (hereinafter referred to as NOx) exhausted therefrom when the fuel is burnt.
  • NOx nitrogen oxides
  • the development of technologies for the reduction of the exhaust of NOx has been pushed forward actively.
  • the fuel for boilers, which produces less pollutants during combustion is liquefied natural gas (LNG) and so on.
  • LNG liquefied natural gas
  • the NOx which is produced when a gaseous fuel with less nitrogen contents is burnt is thermal NOx produced by the oxidation of nitrogen in the air supplied for combustion in a high-temperature atmosphere.
  • thermal NOx highly depends on the temper­ature, and the thermal NOx increases as the flame temperature rises.
  • the flame temperature varies according to the mixing ratio of fuel to combustion air, i.e. the excess air ratio (air quantity/theoretical air quantity), and is highest when the fuel is burnt with an adequate quantity of air (theoretical air quantity), neither excessive nor insufficient, for complete combustion.
  • diffusion combustion is usually performed in an ordinary gaseous fuel boiler.
  • fuel and combustion air are fed through separate nozzles into the furnace, in which they are mixing together to form a flame.
  • This method is featured by the stability of the flame.
  • this combustion method however, during the fuel-air mixing process, there invariably exists a zone where the excess air ratio approaches 1. In this zone, the flame temperature rises, thus generating much NOx.
  • the lean combustion, two-stage combustion, and gas recirculation burning methods have been developed on purpose to reduce the amount of NOx by decreasing the flame temperature.
  • the two-stage combustion and the gas recirculation burning methods are excellent in the effect of NOx reduction, but are liable to discharge unburnt gases. In order to prevent this, the furnace has to be large in size, and therefore, these methods are disadvantageous from an economical point of view.
  • the lean combustion is a combustion under a higher excess air ratio. In this method, since the exess air increases, the heat discharged out of the boiler through the combus­tion gas increases to deteriorate the thermal efficiency of the boiler.
  • a boiler which employs a premixture flame is, for example, disclosed in Japanese Patent Examined Publication No. 52-28251, which uses a two-stage burning combining a diffusion flame with insufficient air and a premixture flame with excess air.
  • This combustion method is very effectively in reducing NOx, but the diffusion flame with an excess air ratio of less than 1 has a long flame form, so that the furnace has to be large.
  • the oxygen in the combustion gas burnt with excess air must be used. To this end, it is necessary to provide for them time enough to be mixed, so that the boiler has to be made large.
  • a boiler according to this invention has in a furnace a heat transfer pipe for heating water to produce steam due to combustion heat of a gaseous fuel burner means, a steam drum communicating with the heat transfer pipe for accumulating steam sent therefrom, an exhaust gas duct through which combustion gas is exhausted, and means provided in the exhaust gas duct for burning unburnt gaseous fuel.
  • the gaseous fuel burner means includes a nozzle for injecting premixture of a gaseous fuel and air into a furnace. It further includes flame holding means which is provided near the outlet of the nozzle to divide the premixture into two flows and generate a circulating flow between the flows.
  • the premixture burner with flame holding means can stabilize the flame and restrain the generation of NOx. Even if unburnt gas remains, it is burnt as it flow through the exhaust gas duct, so that a reduction of NOx can be attained for the boiler as a whole.
  • the flame of the premixture burner is shorter than the diffusion flame, and therefore, the boiler need not be made large in size.
  • the nozzle for injecting a premixture of gaseous fuel and air into the furnace preferably has a fuel passage, a combustion air passage, and rectifying means disposed in a region where these passages converge into a single passage and in a region where the fuel and air are mixed to form a single mixture flow.
  • the fuel-air mixture is preferably fed in a straight-line flow into the furnace.
  • the flame holding means is preferably a plate provided not parallel to a flow direction of the mainstream of the fuel-air mixture.
  • the gaseous fuel burner means includes a diffusion flame burner having nozzle from which gaseous fuel and air are injected, respectively and premixture flame burners which inject fuel-air mixture, so that when the boiler is started up, a diffusion flame is formed and as the boiler load increases, the premixture flame burners inject the premixture.
  • the flame holding means is preferably a plate having an area smaller than a cross sectional area of the nozzle, this is disposed at an outlet of the nozzle not parallel to a flow direction of the main­stream of the mixture.
  • the flame holding means ensures that combustion of the mixture starts at a central portion of the flow of the mixture and that a part of the combustion gas is mixed in the mixture at the outer periphery of the mixture flow before the mixture starts to burn.
  • a suitable gaseous fuel burner preferably has a nozzle for injecting premixture into a furnace in a straight flow, which is obtained by mixing fuel with air in advance of feeding them into the furnace.
  • the burner also has a plate having an area smaller than the nozzle cross-sectional area, provided at the outlet of the nozzle not parallel to the flow direction of the mainstream of the mixture, whereby the mixture starts to burn from the central portion of the mixture flow and a part of the combustion gas is mixed in the mixture at the outer periphery of the mixture flow before the mixture starts to burn.
  • the burner further has a diffusion combustion burner for injecting fuel and air through the respective nozzles.
  • the combustion gas from the outer periphery of the mixture can be mixed in the mixture before the mixture burns at the end of the mixture.
  • the burner for gaseous fuel can be provided with a primary nozzle for injecting gaseous fuel-air mixture, a primary combustion chamber outer wall in a cylindrical or conical form provided on a portion of the primary nozzle close to the furnace to define a primary combustion chamber therein, and a secondary nozzle for injecting combustion air, provided concentric with the the primary combustion chamber outer wall.
  • the air ratio of the premixture from the primary nozzle should be 0.5 to 0.9 and the air ratio of the premixture from the secondary nozzle should be 1.0 to 1.5, and, above all, the total air ratio of the primary and secondary nozzle should be 1.0 to 1.2.
  • the combustion gas introduced to the center of the mixture ignites the mixture due to heat transfer, thereby stabilizing the flame.
  • an ignition method such as this, the flame spreads from the center portion of the mixture to the outside thereof.
  • the combustion gas comes to be mixed in the mixture at the outer periphery thereof and the high-temperature range of the flame is restricted, so that the production of thermal NOx is restrained.
  • the flame holder is disposed not parallel to the direction of the mainstream of the fuel-air mixture and to collide with the mixture, thereby generating a circulating low of high-temperature combustion gas in a downstream side of the flame holder.
  • One of means for facilitating the mixing the combustion gas from the outer periphery of the mixture flow with the mixture is preferably a combustion which can circulate the combustion gas near the outlet of the mixture nozzle. To this end, it is desirable to make a space to which the mixture is injected larger in diameter than the fuel-air mixture flow.
  • the disclosed combus­tion is a gas turbine combustor.
  • a flame holder is disposed in the center of the mixture flow, but the relationship between the diameters of the mixture nozzle and the combustor is not described.
  • a combus­tion method (of a gas turbine) disclosed in USP 3,961,475, the mixture is injected radially, and then accumulates near the wall of the combustor. Therefore, the flame is formed from the combustor wall, resulting in an insufficient introduction of the combustion gas from the outside of the mixture flow.
  • the premixture flame is generally unstable and has a narrow range of stable combustion compared with the diffusion flame.
  • a premixture flame When a premixture flame is adopted and a single burner is provided, it is preferable to provide a primary combustion chamber in the burner to realize a low NOx combustion under high load.
  • the combustion In the primary combustion chamber, the combustion is occurred with a low air ratio as low as 0.5 to 0.9 and then the unburnt gas therefrom can be burnt completely by the remaining oxygen injected from the secondary nozzle.
  • a burner comprises a cylindrical diffusion flame burner 6 disposed in a central portion and a plurality of premixture flame burner apparatus 1000 disposed around the diffusion flame burner 6.
  • the diffusion flame burner 6 has a fuel nozzle 11 disposed in a center thereof and air nozzles 10 disposed around the fuel nozzle 11.
  • a multiplicity of heat transfer tubes 117 are disposed adjacent to a furnace wall 999.
  • Inside a burner throat there are provided an ignitor 13 and water pipes 12 for prevention of burning loss of the burner.
  • the premixture flame burner apparatus 1000 comprises six rectangular burners 1000a through 1000f.
  • Each of these burners comprises a premixture injection nozzle 2, an air damper 7, a rectifier plate 3, an air supply pipe 5, and a fuel nozzle 4.
  • the fuel nozzle 4 has a plurality of openings, through which the fuel is dispersed and fed into the air flow.
  • the zone down­stream of the fuel nozzle 4 is the mixing zone.
  • the rectifier plate 3, which is a honeycomb-structured resistor, has a rectifying function to form a flow of a uniform speed distribution and also has a function to prevent a backfire of the premixture flame since the outlet velocity is increased as the passage cross section is reduced here.
  • a strip-shaped flame holder 1 is disposed near the outlet of the nozzle 2 to extend perpendicular to a direction of the mainstream of the mixture.
  • the lengths of the sides of the flame holder 1 are shorter than the corresponding sides of the nozzle. The reason is that if the longitudinal length of the side of the flame holder is longer than that of the corresponding side of the nozzle, a part of the mixture flow is bent and injected at right angles to the mainstream, thereby deteriorating the stability of the flame.
  • the diffusion combustion burner 6 When the boiler is started up, the diffusion combustion burner 6 is used, and as the boiler load is increased, the mixture of fuel and air is injected from the premixture flame bruner apparatus 1000.
  • the premixture flame burner apparatus injects firstly the mixture from one of the six burners 1000a - 1000f, and as the load increases, the mixture is injected from the other burners successively.
  • the dif­fusion flame burner 6 is used to stabilize the premixture flame. However, under the condition that the premixture flame is formed stably, no fuel and air is injected from the diffusion flame burner 6.
  • a fuel nozzle 11 is installed coaxially with the burner 6 and an air nozzle 10 is disposed to surround the fuel nozzle 11.
  • a flame holder 9 is provided above an upper end of the fuel nozzle 11 to stabilize the diffusion flame.
  • a swirl flow generator 8 installed at the air nozzle 10 prometes mixing of fuel and air, thereby shortening the diffusion flame.
  • the premixture flame burner includes the fuel nozzle 4 having a plurality of openings, provided upstream of the premixture injection nozzle 2. The gaseous fuel supplied from the fuel nozzle 4 and air supplied from the air supply pipe 5 are mixed uniformly before the mixture is injected from the premixture injection nozzle 2. The quantity of combustion air is controlled by the air damper 7.
  • the rectifier plate 3 rectifies the flow of air and serves as a flame arrester to prevent a backfire of the premixture flame.
  • the flame holder 1 in a strip form is provided downstream of the premixture injection nozzle 2 to stabilze the premixture flame.
  • the flame holder 1 have an area smaller than the premixture injection nozzle 2.
  • Fig. 3 shows a boilder in which the burner of Fig. 1 is installed.
  • the boiler is a natural circulation type water pipe boiler.
  • Water stored in a water drum 131 is introduced through heat transfer pipes 117 into a steam drum 128.
  • water is sepa­rated from steam and returned to the water drum 131, while the steam is accumulated in a seam reservoir 129.
  • it is desirable that the premixture flow should spread over a space greater than a burner diameter, and that the nozzle injection outlets of the premixture burner apparatus are located flush with the furnace wall.
  • the combustion gas is discharged through an exhaust gas duct 114 to the outside of the boilder. In this process, the unburnt gas is burnt by a combustor 126.
  • the combustion gas flows in a direction opposite to the flow direction of the premixture in the exhaust gas duct 114, and is preheated by a first air preheater 123 and a second air preheater 124 at the front and the rear stages of the unburnt gas combustor 126, respectively.
  • the generation of NOx does not depend on the combustion load and the flame can be shortened. Therefore it becomes possible to rise a heat load of the furnace above 2,000,000 kcal/m3h.
  • the flame length can be normally shortened to less than 50 cm. It is enough that the depth of the furnace is 1 m.
  • the boiler according to this invention can increase a capacity thereof by only expanding the furnace in the longitudinal direction of the water drum and the steam drum to increase the heat transfer area. This can be attained by use of a premixture flame burner with a flame holder because in this case, even if the burner capacity is increased, the flame length hardly changes. Needless to say, by increasing the number of premixture nozzles, the boiler capacity can be increased. Referring with Fig.
  • the fuel supply rate on the axis of ordinate represents in percentage the ratio of the fuel used by the respective nozzle to the fuel used by the boiler when the boiler load is 100%.
  • the nozzle A the premixture burner 1000a with a flame holder
  • the quantities of fuel and air from the diffusion flame burner corresponding to this air ratio are decreased and the quantities of fuel and air corresponding to such decreased quantities are injected from the nozzle A.
  • the quantities of fuel and air injected from the nozzle A are increased.
  • a premixture of an air ratio of 1.1 is injected from the nozzle B (the premixture burner 1000b with a flame holder) at 20 m/s.
  • the premixture injected from the nozzle A is decreased by a quantity of the premixture corresponding to the quantity of the premixture injected from the nozzle B.
  • the similar operation is repeated and the premixture is injected from the nozzle C (the premixture flame burner 1000c with a flame holder), the nozzle D (the premixture flame burner 1000d with a flame holder), the nozzle E (the premixture flame burner 1000e with a flame holder), and the nozzle F (the premixture flame burner 1000f) in that order.
  • the load is changed from 70% to 90%, the quantities of the premixture fed from the nozzles A, B, C and D are changed accordingly.
  • the load reaches 90%, the use of the diffusion flame burner is stopped, and the premixture including the quantities of fuel and air corresponding to those injected from the diffusion flame burner is fed from the nozzles E and F.
  • the load changes from 90% to 100% the quantities of the premixture fed from the nozzles A, B, C, D, E and F are changed accordingly.
  • Fig. 5 shows the result of study into the blowout limit of the premixture flame stabilized by a flame holder disposed downstream of the premixture injection outlets.
  • the axis of abscissa represents the excess air ratio of the premixture and the axis of ordinate represents the injection velocity of the premixture.
  • the white dots indicate the stable combustion of the premixture flame and the black dots indicate that the premixture flame becomes unsatable and blows out. It will be understood that the stable combustion range of the premixture flame stabilized by the flame holder becomes narrower as the excess air ratio increases.
  • Fig. 6 shows the effects of the flame holder on the reduction of NOx of the stabilized premixture flame.
  • the axis of abscissa represents the excess air ratio of the premixture and the axis of ordinate presents the concentration of NOx from the boiler.
  • Fig. 7A shows a burner according to the invention with a flame holder for stabilizing the premixture flame. Near the peripheral edge of the flame holder 1 disposed downstream of a premixture injection outlet 21, there is formed swirls of the premixture as indicated by the arrows, and then an ignition is occurred in this area. After the ignition, as the injection quantity of the premixture is increased, high-temperature combustion products circulate inside and outside the premixture flame 99 as indicated by the arrows.
  • Fig. 7B shows a burner in which the premixture flame is stabilized by means of a pilot flame.
  • the premixture of an excess air ratio of about 1.0 is supplied to the premixture supply pipe 22 to form a stable pilot flame 300 at an annular nozzle provided around the outer periphery of the cylindrical premixture injection outlet 23.
  • the premixture from the premixture inejction outlet 23 receives energy from the pilot flame 300, so that the premixture flame 99 is formed as shown in Fig. 7B.
  • the NOx concentration is compared between the above-mentioned two kinds of premixed flames.
  • the premixture flame with the pilot flame generates NOx of about 800 ppm, while the premixture flame with the flame holder generates NOx of no more than 25 ppm.
  • the concentration of NOx from the premixture flame with a flame holder is about one third of the NOx concentration from the premixture flame with the pilot flame.
  • Fig. 6 The numerals given beside the white dots in Fig. 6 represent combustion loads in units of 104 Kcal/m3h. As can be seen from Fig. 6, even if the combustion load changes between 66 x 104 Kcal/m3h and 267 x 104 Kcal/m3h, the NOx concentration hardly changes. Therefore, by using the premixture combustion method relating to the invention, a high-load and low-NOx boiler can be realized.
  • Fig. 8 shows the effect of the ratio of a combustion inner diameter D3 to the premixture nozzle inner diameter D2 on the concentration of NOx generated from the premixture flame of the premixture flame burner with a flame holder.
  • D3/D2 is smaller than 4
  • the NOx concentration is high. This is considered as follows.
  • the combustor inner diameter D3 becomes small, it becomes difficult for the combustion products to circulate outside the flame, which allows the oxygen partial presssure to increase, thus increasing the NOx concentration.
  • Figs. 9A and 9B show a modification of the burner apparatus for a low-NOx boiler of Fig. 1.
  • the buffer apparatus comprises a cylindrical diffusion flame burner with a flame holder disposed in the center, and an annular premixture flame burner with a flame holder disposed around the diffusion flame burner.
  • the premixture flame burner is composed of four nozzles 2a, 2b, 2c and 2d, into which an annular flow passage is divided.
  • Each nozzle has a fuel-air mixing zone disposed upstream of the injection outlet 21 and a mixture rectifier 3 located between the mixing zone and the injection outlet 21.
  • the fuel is diffused through the fuel nozzle having a plurality of outlets into the air flow to be mixed together.
  • the rectifier 3 is a flow-passage resistor of honeycomb structure.
  • At each nozzle outlet a strip-shaped flame holder 1 is so disposed as to extend perpendicular to the direction of the flow of mixture.
  • the sides of the flame holder are shorter than the corresponding sides
  • the diffusion combustion burner disposed in the center of the burner is used firstly, and as the boiler load is increased, the fuel-air mixture is injected from the premixture burner with the flame holder.
  • the mixture is at first injected from one of the four nozzles, and as the load increases, the premixture is injected from the other nozzles in succession.
  • the diffusion flame burner is used to stabilize the pre­mixture flame. However, under the condition that the premixture flame is formed stably, the injection of fuel and air from the diffusion flame burner is stopped.
  • Fig. 10 shows a relation between the boiler load equipped with the low-NOx burner of Figs. 9A and 9B and the fuel supply rate from each nozzle.
  • the fuel supply rate on the axis of ordinate represents the ratio of the fuel used by each nozzle to the fuel used by the boiler when the boiler load is 100% in percentage.
  • a boiler load of 20% only the diffusion flame burner is used, and when the load reaches 20%, fuel and air are fed through the nozzle A, an arbitrary one of the four nozzles.
  • the fuel and air injected from the diffusion flame burner is reduced by quantities thereof corresponding to those injected from the nozzle A, and fuel and air thus reduced are injected from the nozzle A.
  • the fuel and the air injected from the nozzle A are increased until the boiler load reaches 30%, and when 30% is reached, the premixture of air ratio of 1.1 is injected at the velocity of 20 m/s from the nozzle B, another arbitrary one of the remaining three nozzles.
  • the premixture injected from the nozzle A is reduced by a quantity of the premixture corresponding to that of the premixture injected from the nozzle B.
  • the similar operation is repeated. Namely the premixture is injected from the nozzle C, an arbitrary one of the remaining two nozzles when the load is 50% and the premixture is injected from the nozzle D, the last one of the four nozzles when the load is 70%.
  • the load reaches 90%, the use of the diffusion flame burner is stopped, and the nozzles A and B inject the quantity of the premixture corresponding to the quantities of fuel and air which have been injected from the diffusion flame burner.
  • the quantities of the premixture injected from the nozzles C and D are changed accordingly.
  • Fig. 11 is another modification of the low-­NOx burner of Fig. 1.
  • This embodiment features the use of hemisphere Venturi portions 27 as rectifying means to form a uniform premixture of gaseous fuel and combustion air.
  • the consturction except for the Venturi portions 27 is the same as in Figs. 9A and 9B.
  • Figs. 12a and 12B show the construction of a burner apparatus for a low-NOx boiler, having a plurality of cylindrical premixture nozzles.
  • the burner apparatus comprises a first cylidnrical diffusion flame burner 6 for ignition disposed at the center thereof, and a plurality of premixture flame burners 1000 each having a flame holder, disposed to surround the diffusion flame burner 6.
  • Each of the premixture flame burners 1000 has a second cylindrical diffusion flame burner 600 for ignition disposed coaxially with the injection outlet 32 of the premixture nozzle.
  • a fuel nozzle 35 is provided coaxially with an axis of the burner, and an air nozzle 36 is disposed around the fuel nozzle 35.
  • the air nozzle 36 has a swirl flow generator 37 mounted therein so as to control the swirl strength of combustion air.
  • the premixture flame burner 1000 has a fuel nozzle 39 for premixture combustion disposed upstream of the premixture injection outlet 32.
  • the gaseous fuel from the fuel nozzle 39 and the combustion air from an air supply pipe 40 are mixed to form a uniform premixture through a Vnnturi portion 41.
  • the second diffusion flame burner 600 is disposed coaxially with the pre­mixture injection outlet 32, and a fuel nozzle 45 is disposed coaxially with the diffusion flame burner 600.
  • An air nozzle 46 is disposed to surround the fuel nozzle 45.
  • the air nozzle 46 is provided with a swirl flow generator 44 which serves to shorten the diffusion flame of the second diffusion flame burner.
  • the second diffusion flame burner ignites the whole of the premixture.
  • the above-mentioned two kinds of diffusion flames are used to ignite the premixture when the boiler load is changed.
  • a flame holder 31 At an upper end of the air nozzle 46, there is provided a flame holder 31.
  • the flame hodler 31 causes a circulating flow of the premixture to near the peripheral edge of the flame holder, thereby improving the stability of the premixed flame.
  • the flame holder 31 causes combustion products to be circulated inside and outside the flame, so that NOx can be reduced.
  • Figs. 13A and 13B show a modification of the burner for a low-NOx boiler, provided with a plurality of cylindrical premixture injection outlets.
  • the burner comprises a first cylindrical diffusion flame burner 6 for ignition and a plurality of premixture flame burners 1000 disposed surrounding the diffusion flame burner 6.
  • the burner 1000 has fuel nozzle 60 for the second diffusion flame provided coaxially with the axis of the premixture outlet 48.
  • the first diffusion flame burner 6 has a fuel nozzle 49 provided coaxially therewith and an air nozzle 50 surrounding the fuel nozzle 49.
  • the air nozzle 50 has a swirl flow generator 54 installed therein to control the swirl strength of the combustion air.
  • a fuel nozzle 55 for premixture combustion is disposed upstream of the premixture injection outlet 48.
  • the fuel from the fuel nozzle 55 and the combustion air from the air supply pipe 56 are mixed to form a uniform premixture by the swirl flow generator 57.
  • rectifying means 59 which serves to form a uniform speed distribution of the premixture in the radial direction of the outlet 48.
  • a fuel nozzle 60 for the second diffusion flame is disposed coaxially with the outlet 48.
  • the above-mentioned two types of diffusion flames are used to ignite the premixture when the boiler load is changed.
  • a flame holder 47 At a position downstream of the premixture injection outlet 48, there is provided a flame holder 47, which causes a circulating flow of the premixture near the peripheral edge of the flame holder, thereby improving the stability of the premixture flame. Further additionallymore, the flame holder 47 causes combustion products to be circulated inside and outside the flame, so that NOx can be reduced.
  • Figs. 14A shows the pressure, distribution along the radial direction of the premixture injection outlet 48 measured by the Ditot tube
  • Fig. 14B shows the speed distribution of the premixture along the radial direction of the outlet 48.
  • a flared peripheral edge of a flame holder 47 is located at 20 mm in radial direction from the axis of the holder 47, while a base peripheral edge of the holder 47 is located at 10 mm in the radial direction.
  • a peripheral edge of the pre­mixture injection outlet 48 is lcoated at about 33 mm in the radial direction from the axis of the holder 47.
  • solid lines indicated by reference numerals 61 and 63 represent the pressure and the speed distributions when no rectifying means is provided
  • broken lines indicated by reference numerals 62 and 64 represent the pressure and the speed distributions when a honeycomb structure is installed as rectifying means.
  • a negative pressure zone is spread up to a radial position about 20 mm from the axis of the holder 47 due to the action of the swirl flow generator 57.
  • Fig. 14A when no rectifying means 59 is provided (the solid line 61), a negative pressure zone is spread up to a radial position about 20 mm from the axis of the holder 47 due to the action of the swirl flow generator 57.
  • Fig. 14A when no rectifying means 59 is provided (the solid line 61), a negative pressure zone is spread up to a radial position about 20 mm from
  • the premixture when no rectifying means 59 is provided (the solid line 63), the premixture accumulates near the outer periphery of the outlet 48 due to a centri­fugal force caused by the swirl flow generator 57, so that the premixture is not accumulated above the flame holder 47. Consequently, the premixture flame is located at the outer periphery of the outlet 48.
  • the high-temperature exhaust gas caused by the premixture flame is drawn into the negative pressure zone extending around the center portion of the outlet 48, so that a flame is formed from within the outlet 48. Raised is a problem that the flame holder 47 deteriorates as it it heated from the upstream side thereof.
  • Fig. 15 corresponds to a horizontal sectional view of the boiler of Fig. 3.
  • a furnace 112 comprises a plurality of radiant heat transfer pipes 115a arranged mutually adjacent on the upsteam side (left side in Fig. 15) to form a furnace front wall 180a, radiant heat transfer pipes 115b and 115c arranged to form walls extending from the opposite ends of the furnace front wall 180a and extending perpendicular thereto towards the downstream side (right side in Fig. 15) so that a combustion chamber is defined therebetween, steam generating pipes 116c and 116d arranged as extensions, on the downstream side, from the walls formed of the radiant heat transfer pipes 115b and 115c, and steam heat transfer pipes 117 located between walls of the stream generating pipes 116c and 116d.
  • a steam drum 128 extending from the upstream to the downstream of the furnace 112.
  • a water drum 131 in parallel with the steam drum 128.
  • the radiant heat transfer pipes 115a, 115b and 115c are connected at their lower ends with the water drum 131 and at their upper ends with the water phase in the steam drum 128.
  • a steam distribution pipe 132 In the center of the furnace bottom between the walls of the steam generating pipes 116c and 116d, there is a steam distribution pipe 132 on the extension of the axis of the water drum 131.
  • each of the radiant heat transfer pipes 115b and 115c and the steam generating pipes 116c and 116d is integrally provided at upstream and downstream sides with plates 169.
  • the adjacent flat plates 169 are partially overlapping each other to constitute the furnace side walls 180b and 180c.
  • heating passages 170a and 170b On the downstream portion of the furnace 112, there is heating passages 170a and 170b separating hori­zontally to the left and right sides.
  • the heating passages 170a and 170b are defined by a radiant heat transfer pipe 115d, radiant heat transfer pipes 115f and 115e, steam heat transfer pipes 117, steam generating pipes 116a and 116b, downcast pipes 120a and 120b, and steam generating pipes 116c and 116d.
  • the pipe 115d is located spaced from the steam generating pipes 116c and 116d constituting the downstream-side end portions of the furnace side walls 180b and 180c and the pipe 115d also constitutes a heating-passage rear wall 180d parallel with the furnace front wall 180a and wider than the furnace front wall 180a.
  • the radiant heat transfer pipes 115e and 115f extend from the opposite ends of the boiler rear wall 180d towards the upstream side and constituting part of the heating-passage side walls 180e and 180f parallel with the furnace side walls 180b and 180c.
  • the steam heat transfer pipes 117 are, on the extreme downstream side, disposed between the furnace side walls 180b and 180c.
  • the steam generating pipes 116a and 116b are disposed adjacent to the radiant heat transfer pipes 115e and 115f and constitute part of the heating passage side walls 180e and 180f.
  • the downcase pipes 120a and 120b are disposed between the steam generating pipes 116a and 116b and constitute part of the boiler side walls 180e and 180f.
  • the steam generating pipes 116c and 116d constitute part of the furnace side wall 180b and 180c.
  • the radiant heat transfer pipes 115d, 115e and 115f are connected at their lower ends to the water drum 131 and at their upper ends to the water phase in the steam drum 128.
  • the steam generating pipes 116a, 116c, 116b and 116d arranged in a plane intersecting perpendicularly to the furnace side walls, are communicated with one another to form a single pipe line via the respective bent portions.
  • the steam generating pipes 116c and 116d are connected at their lower ends to the steam distributing pipe 132, and the steam generating pipes 116a and 116b constituting the heating passage side walls are connected at their lower ends to a water reservoir 133.
  • the reservoir 133 is arranged on the lower furnace side of the heating passage side walls 180e and 180f and along these side walls 180e and 180f.
  • the steam generating pipes 116a and 116b have pipe sections bending a number of times up and down between the boiler side walls 180e and 180f and the steam generating pipes 116c and 116d consti­tuting the furnace side walls 180b and 180c. Therefore, the passages in the steam generating pipes 116a and 116b communicate through the steam generating pipes 116c and 116d with the steam distributing pipe 132.
  • the steam heat transfer pipes 117 are connected at their upper ends to the steam reservoir 129 and at their lower ends to the steam distributing pipe 132.
  • the heating passages 170a and 170b there is superheaters 118 forming a single bent pipe comprising a plurality of pipes interconnected each other.
  • the superheaters 118 are connected at one ends thereof to the steam phase of the steam drum 128 through steam pipes 130, and at the other ends thereof to steam-applied equipment, not shown, such as a steam turbine and a chemical plant.
  • Downcast pipes 120a and 120b are provided adjacent to the heating-passage side walls 180e and 180f and on the extensions towards the furnace front walls 180a, respectively.
  • the downcast pipes 120a and 120b constitute flue side wals 180g and 180h parallel with the furnace wall side walls 180c and 180d and continuous on the extensions of the furnace front walls 180a.
  • Downcast pipes 120c and 120d are arranged in the opposite extensions of the furnace front walls 180a to constitute flue front wall 180j and 180k.
  • a flue 114a is defined by a flue top plate 134 provided above the furnace side wall 180b, the flue side wall 180g, the flue front wall 180j, and the steam generating pipes 116a and 116c, and a flue bottom plate 135 provided below the steam generating pipe 116a.
  • a flue 114b is defined by a flue top plate 134 provided above the furnace side wall 180c, the flue side wall 180h, the flue front wall 180k, and the steam generating pipes 116b and 116d, and a flue bottom plate 35 provided below the steam generating pipe 116b.
  • convection heat transfer pipes 119 are provided, for example, in 20 rows, each having five pipes 119.
  • the convection heat transfer pipes 119 are connected at their upper ends to the water phase of the steam drum 128, and at their lower ends to the water drum 131.
  • the downcast pipes 120a and 120c communicate at their lower ends with the water drum 131 and at their upper ends with the water phase of the steam drum 128.
  • Return pipes, not shown, are provided, which communicate between the bottom part of the steam reservoir 129 within the steam drum 128, and the water reservoirs 133.
  • the return pipes are installed such that they are inclined from the steam reservoir 129 to the water reservoirs 133 to ensure that there is no air pocket in the midway thereof.
  • upper flues 114c and 114d are provided at the substantially same height as the steam drum 128 and in parallel with the steam drum 128.
  • the flues 114a and 114b communicate with the upper flue 114c and 114d, respectively, through openings made in the flue top plate 134.
  • the upper flues 114c and 114d are constructed symmetrically. So, description will be made only on the upper flue 114d.
  • Combustion gas rises from the flue 114b through the above mentioned openings, and flows through the upper flue 114d in the direction opposite to the combustion gas flow in the flue 114b.
  • the upper flue 114d includes a second air preheater 124 provided downstream of the openings, an unburnt gas combustor 126 provided downstrem of the second air preheater 124, and a first air pre­heater 123 provided downstream of the unburnt gas combustor 126.
  • the first air preheater 123 and the second air preheater 124 are almost identical in constuc­tion.
  • Each preheater comprises tube plates 171 provided at the opposite ends in the direction of the combustion gas flow, a plurality of round pipes constituting a smoke duct communicating between the tube plates 171, and baffle plates 172, the number of which is odd, provided between the tube plates 171 (for example, three plates 172 for the first air preheater and one plate 172 for the second air preheater).
  • These smoke ducts serve as means for rectifying the flow of the exhaust gas.
  • the unburnt gas combustor 126 oxidize carbon monoxide, which is the unburnt gas in the exhaust gas, to be carbon dioxide.
  • the unburnt gas combustor 126 was made by catalyst for accelerating reaction in a plate form and disposed almost in parallel with the flow of the exhaust gas in the passage of the exhaust gas. Used is the catalyst with an active temperature in the range of 300° to 1000°C.
  • the catalyst need not be in a plate form but may be in a grill form. It is also pos­sible to use spheroidal bodies about 3 mm in diameter as carriers of catalyst and make spheroidal catalyst.
  • the spheroidal catalyst may be filled in the exhaust gas passage.
  • an air supply duct 122b is arranged in parallel with the upper flue 114d.
  • the upper flue 114d and the air supply duct 122b are adjacent to each other through the intermediary of the upper flue side plate 114f.
  • the baffle plates of the first air preheater 123 which include the one adjacent to the tube plate 171, are alternately extended into the inside of the air supply duct 122b, thereby interrupting the passage of the air supply duct 122b.
  • a heating control valve 125 comprising a flat plate supported by the top surface and the bottom surface of the air supply duct 122b and formed integrally with a rotatable post. This heating control valve 125 controls the quantity of air flowing into the second air pre­heater.
  • the angle between the flat plate and the longitudinal direction of the air supply duct 122b can be controlled to change the passage cross section of the duct 122b.
  • the upper flue side plate 114f is not provided at the adjoining part of the first and second air preheaters, and the air supply duct 122b. Therefore, gas can flow freely between them.
  • One end portion of the air supply duct 122b close to a flue front wall 180k is extended to the opposite side of the flue 114b of the flue front wall 180k, and communicates with a window box 173 formed around the periphery of a burner throat 143 provided in the furnace front wall 180a outside the furnace.
  • the other end portion of the duct 122b communicates to a blower apparatus (not shown).
  • the window box 173 is provided coaxially with the burner throat 143, and is surrounded by a cylindrical burner outer wall 145 larger in diameter than the burner throat, and a burner side wall 147 forming an end face of the cylinder.
  • a burner 111 is provided at the center of the window box 173.
  • the burner 111 includes a primary combustion chamber 157 at the center thereof.
  • the primary combus­tion chamber 157 comprises a main mixture passage 212 located on the upstream side and serving as the main nozzle for forming a main combustion flame of an air ratio of 1 or less, an annular stabilizer plate 155 having pilot flame holes 156 each forming a pilot flame located to surround the main premixture passage 212, a primary combustion chamber side wall 217 disposed at the outer periphery of the stabilizer plate 155 to constitute an upstream side wall of the primary combustion chamber 157, a wall surface formed of water cooling pipes 158 disposed at the outer periphery of the primary combustion chamber side wall 217, and a cylindrical primary combustion chamber outer wall 142 provided contiguous at one end thereof on the upstream side to the wall surface formed of water cooling pipes 158 and loosely extending at the other end thereof into the burner throat 143 and facing the furnace.
  • a secondary combustion chamber 240 is formed on the downstream side of the primary combustion chamber 157.
  • the secondary combustion chamber 240 is continuous on the upstream side thereof to the primary combustion chamber 157, and opened on the downstream side thereof to the furnace 112.
  • a wall of the secondary combustion chamber 240 which connects an axial end portion thereof opened to the primary combustion chamber 157 and the other axial end portion thereof opened to the furnace 112, is provided with the burner throat 143 and an annular auxiliary mixture passage 238 defined between a nozzle 237 forming an inner surface of the burner throat 143 and a nozzle 236 having the end portion of the primary combustion chamber 142 closer to the furnace.
  • the burner thoat 143 and the auxiliary mixed gas passage 238 are provided such that the cross section of the secondary combustion chamber 240, which is perpendicular to the axis of the burner, increases towards the furnace.
  • the auxiliary mixture passage 238 is opened at one end thereof to the secondary combustion chamber 240.
  • the other end of the passage 238 communicates with air supply ducts 122a and 122b through the damper 232 and the window box 173.
  • discs 160 and 235 are provided, respectively.
  • a plurality of resistor type swirl vanes 162 are mounted in an annular space defined between the discs 160 and 235.
  • Each vane is provided integrally with a support post 161.
  • the post 161 is mounted with its axis parallel with the generating line of a cylinder constituting the primary combustion chamber 142, and the opposite ends of the pots 161 are rotatably born in bearing holes formed in the discs 160 and 235.
  • a plurality of fuel injection holes 251 are connected to a fuel reservoir to which gaseous fuel is supplied, through a gas reservoir 252 in the vane 162, and a supply pipe passing through the central part of either one of the support posts 161 on the furnace side and the side closer to the burner side wall 147 and also through a communicating pipe 234.
  • the damper 232 is attached integrally to the upstream side ends of the discs 160 and 235. Attached to the upstream side of damper 232 is a movable damper 231 formed integrally with a control rod 230 passing through the burner side wall.
  • Each of the damper 232 and the movable damper 231 has a plurality of circular apertures.
  • the area of the apertures projected in the downstream direction is controlled.
  • the area of the apertures is maximum, so that the air flow rate into the auxiliary mixture passage is maximum.
  • the dampers 231 and 232 are controlled so that the apertures of the movable damper 231 do not coincide with the apertures of the damper 232, the area of the aperture is minimum, so that the air flow rate into the auxiliary mixture passage is minimum.
  • Descrip­tion has been made to the movable damper 231 which has a plurality of apertures, but it is also possible to achieve the same object by use of a movable damper 231 which is made of a disc plate without apertures.
  • the main mixture passage for forming a main flame is provided on the inner periphery of the stabilizer plate 155 for forming a pilot flame.
  • the main mixture passage is an annular passage defined by a primary throat 210 and a premixture throat 140 provided to surround the outer periphery of the primary throat 210.
  • the upstream side of the primary throat 210 is connected to a nozzle 208 having an arc cross section.
  • the upstream side of the premixture throat 140 is connected to a nozzle 209 having an arc cross section.
  • the end face of the upstream side of the nozzle 208 is connected to the burner side wall, while the end face of the upstream side of the nozzle 209 is connected to a premixture side wall 211 provided on a side of the burner side wall 147 which is closer to the furnace.
  • a plurality of resistor type swirl vanes 206 are mounted in an annular space defined by the burner side wall 147 and the premixture side wall 211.
  • Each vane is provided integrally with a support post 207.
  • the post 207 is mounted with its axis parallel with the generating line of a cylinder constituting the primary combustion chamber outer wall 142, and the opposite ends of the post 207 are rotatably born in bearing holes formed in the burner side wall 147 and the premixture side wall 211.
  • the post 207 is mounted to the vane 206 near the downstream side thereof. Therefore, even if the inclination angle of the vane 206 is increased to rise the swirl strength, it does not occur that the adjacent vanes contact one another and the opening area of the outlet of the vane is decreased.
  • the upstream side end face of the premixture side wall 211 is connected to one end of a damper 205 disposed concentrically with the primary combustion chamber outer wall 142.
  • the other end of the damper 205 is connected to the burner side wall 147.
  • a movable damper 204 formed integrally with a control rod 203.
  • the damper 205 and the movable damper 204 have the construc­tion and operation similar to those of the damper 231 and the movable damper 232.
  • each fuel pipe 201 passing through the nozzle 208.
  • the injection hole 202 is opened at downstream side thereof to the main mixture passage.
  • the injection hole 202 is connected at upstream side thereof to a fuel pipe 179 through the fuel pipes 201 and a fuel reservoir 200 connected to the plurality of fuel pipes 201.
  • the primary throat 210 holds a cylinder 215 at the inner periphery thereof.
  • a flow speed control valve 216 is connected to the furnace side of the cylinder 215.
  • the valve 216 at the upstream side thereof, has a diameter equal to the diameter of the cylinder 215 and the diameter of the value 216 increases towards the furnace.
  • the valve 216 is born to be movable in the direction of the generating line of the primary combustion chamber outer wall 142 by means of the primary throat 210, the cylinder 215, and a blind plate 213 attached to the nozzle 208 and having in the center thereof a guide for a flow speed control rod 214.
  • the flow speed control rod 214 is connected integrally with the cylinder 215 and controls the flow velocity control valve 216.
  • valve 16 When the valve 16 is moved to the upstream side (the state as indicated by the solid line in Fig. 20), the passage area of the main mixture passage 212 facing the primary combustion chamber 157 is minimized.
  • the flow velocity control valve 216 when moved to the downstream side (the state indicated by the broken line in Fig. 20), maximizes the passage area of the main mixture passage 212 facing the primary combustion chamber 157.
  • the flow speed control valve 216 operates according to the quantity of mixture supplied to the main premixture passage 212 to control the passage area of the main premixture passage, which is closer to the primary combustion chamber 157. For example, it is possible to make the speed of the premixture injected from the main premixture passage 212 generally constant, irrespective of the supply flow rate of the premixture. Therefore, it is possible to prevent the flame from withdrawing into the main mixture passage under a combustion condition with low load and reduced supply of premixture.
  • the volume flow rate of air varies according to the preheating temperature. If the flow speed control valve 216 operates so that the cubic expansion can be compensated by measurement of a preheating temperature of air, the outlet speed of the main mixture can be maintained constant irrespective of the preheating temperature. Also, by attaching a flame holder to the flow speed control valve 216, the main combustion flame can be made more stable.
  • the relative position of the movable damper 204 and the damper 231 is changed, so that the area of apertures obtained by mutual overlapping of the movable damper 204 and the damper 231 is changed accordingly. More specifically, as the movable damper 204 changes its position, it changes the area of the apertures, thereby controlling the quantity of air flowing into the main mixture passage 212 or the auxiliary mixture passage 238.
  • the pressure loss in the vanes which occurs when the inclination angle of the vane 206 or 162 is changed. Therefore, the incoming air flow rate varies according to the swirl strength.
  • the fuel supplied from the fuel reseroir 233 flows through the communicating pipe 234, the support post 161 and the gas reservoir 252 held within the vane 162, and injected from a plurality of fuel injection holes 251 provided at the downstream side end face of the vane 162.
  • the injected fuel is mixed with air fed to the auxiliary mixture passage 238, thus forming premixture, which becomes an auxiliary combustion flame.
  • the method of injecting gaseous fuel from the fuel injection holes 251 of the vane 162 can shorten the time necessary for mixing of the air and the gaseous fuel, as compared with the method of mixing the gaseous fuel in the air, which fuel is injected from the fuel pipe 201 extending into the passage. Therefore, the auxiliary mixture passage can be shorter than the main mixture passage.
  • a swirl 254 formed after the swirl vane has a greater intensity of turbulence than that of the downstream side of the fuel pipe 202.
  • the injected gaseous fuel is drawn into the swirl 254 and then mixed completely with the air by small swirls generated by the swirl 254. the mixing of gaseous fuel and air is further promoted in case that the intensity of turbulence is increased by providing protrusions on the surfaces of the vane.
  • the swirl flow formed by the vane is not damped by obstacles.
  • Fuel is separately supplied to form a main combustion flame and an auxiliary combustion flame.
  • the boiler cuts off a supply of fuel to the auxiliary mixture passage.
  • the stabilizer plate 155 injects premixture of an air ratio of 1 or more preferably 1.0 to 1.5 at a few meters per second, preferably 1 to 3 m/s into the primary combustion chamber 157 to form a pilot flame of the premixture.
  • the main combustion mixture passage injects premixture of an air ratio of 1 or less, preferably 0.5 to 0.9 at 20 to 50 m/s in a swirl flow manner into the primary combustion chamber 157, which is ignited by the pilot flame to form the main combustion flame.
  • the auxiliary combustion mixture pasage injects premixture of an air ratio of 1 or more, preferably 1.0 to 1.5 at the 20 to 20 m/s in a swirl flow manner into the secondary combustion chamber 240, which is ignited by the main combustion flame to form the auxiliary combus­tion flame. Since the air ratio of the premixture forming the main combustion flame is 1 or less, the maximum temperature of the flame is lower than the conventional diffusion flame, so that the production of thermal NOx is restrained. At the same time, the thermal NOx produced by combustion is subjected to vapor-phase reduction by intermediate products of the gaseous fuel and reduced to nitrogen. The intermediate products by the main combustion flame vapor-phase reduce the thermal NOx produced by the auxiliary combustion flame into nitrogen.
  • the vapor-phase reduction of the NOx produced by the auxiliary combustion flame due to the main combustion flame is promoted by providing the primary combustion chamber with an angled portion so as to let the mixture from the auxiliary mixture passage smash into the main combustion flame. Since the cross section of the secondary combustion chamber in the flow direction increases towards the furnace, there is no rise in speed in the secondary combustion chamber where the main combustion flame and the auxiliary combustion flame are formed.
  • pilot flame description has been made to a case where it is formed by premixture.
  • the object of the pilot flame lies in igniting the main combustion mixture to form a main combustion flame. Therefore, the method of forming a flame by injecting a small quantity of fuel into the primary combustion chamber and air into the fuel from around thereof, that is to say, the method of forming a pilot flame by the diffusion flame does not deviate from the object of the present invention.
  • gaseous fuel is divided into three portions, which are separately supplied to form a pilot flame, a main combustion frame and an auxiliary combustion flame. And the ignition is caused to take place successively by the flames in the above-mentioned order.
  • the gaseous fuel may be divided into more than three portions, if possible.
  • the radiant heat transfer pipe 115b is abutted onto the furnace 112 and the flue 114a, while the radiant heat transfer pipe 115c is abutted onto the furnace 112 and the flue 114b.
  • the surface temperature of the sides of the radiant heat transfer pipes 115b and 115c closer to the flues becomes substantially equal to the exhaust gas temperature in the flues. Therefore, the heat quantity escaping to the outside from the sides of the radiant heat transfer pipes which are apart from the furnace is reduced compared with the conventional techniques in which the sides of the radiant heat transfer pipes which are apart from the furnace are covered by heat insulators.
  • the thermal efficiency of the boiler is improved.
  • the convection heat transfer pipes 119 are disposed in a plural number in the direction not in parallel with the flow direction of the combustion gas, the flow near the surface of the convection heat transfer pipes 119 is kept in a turbulent state, whereby the heat transfer rate is raised. Also, it has become possible to secure a heat transfer area necessary for a boiler with an evaporation rate of several tons/h to several hundred tons/h in a limited furnace volume.
  • the steam heated as it flows through the steam heat transfer pipes 117 is flowed into the steam reservoir 129 in which the steam is heat-transferred with the water in the steam drum 128 through the pipe wall of the steam reservoir 129 placed in the water of the steam drum 128.
  • the steam heats the water in the steam drum and is condensed into the condensate.
  • the condensate flows bakc to the water reservoir 133 through a return pipe (not shown).
  • the condensate from the water reservoir 133 is heated to evaporate as it passes through the steam generating pipe 116a or 116b, and is further heated to the steam by the flame in the radiant heat transfer pipe 116c and the steam heat transfer pipes 117, or in the radiant heat transfer pipe 116d and the steam heat transfer pipes 117.
  • the steam then flows into the steam reservoir 129 incorporated within the steam drum 128, where the steam transfers the heat to the water held in the steam drum 128.
  • the heat transfer 45,000 to 60,000 kcal/m2h, 1.5 to 2 times higher than the conventional method by a combination of movement and condensation of heat transfer medium without a damage of theat transfer pipes or burning loss thereof due to contact with the flame.
  • the superheaters 118 installed in the heating passages 170 prevent combustion gas from deviating and breaking away the combustion gas from a wall surface of the bent passages of the heating passages 170, and uniform the velocity of the combustion exhaust gas at the inlet of the flues 114. According this, the heat exchange efficiency in the flues 114 is improved. Further, there is no heat transfer pipes having locally high heat absorption and then the damage to the pipes such as burning loss is prevented.
  • the second air preheater 124 provided at the uppermost side of the upper flue 114d receives the air with its incoming flow rate controlled by the opening adjustment of the heating control valves 125. In this way, the heat quantity is controlled which is deprived of the combustion exhaust gas in the second air preheater 124. As a result, the temperature of the combustion exhaust gas to be flowed into the unburnt gas combustor 126 is maintained in the range which is set according to the active temperature of the catalyst used in the unburnt gas combustion 126.
  • the combustion exhaust gas temperature at the inlet of the unburnt gas combustor 126 can be maintained in the set temperature range even if the boiler load changes.
  • the second air preheater 124 is located against the upstream side of the unburnt gas combustor 126.
  • the combustion exhaust gas is rectified as it passes through the flue of the second air preheater 124 and flows into the unburnt gas combustor 126.
  • the unburnt gas combustor 126 can reduce the concentration of carbon monoxide which is the unburnt gas in the combustion exhaust gas by controlling the time duration of contact between the combustion exhaust gas and the catalyst.
  • the contact time duration is set 0.1 to 1 sec/ond, the carbon monoxide concentra­tion could be reduced from several thousands ppm to 100 ppm or less.
  • the unburnt gas combustor may be applicable, which burns a small amount of gaseous fuel in the exhaust gas to generate a high temperature gas which is brought into contact with carbon monoxide to oxidize it into carbon dioxide.
  • Fig. 19 is a characteristic diagram showing relations between the concentration of oxygen and those of NOx and carbon monoxide contained in the combustion exhaust gas at the outlet of the boiler.
  • the solid lines indicate the characteristics of the conventional boiler and the broken lines indicate the characteristics of the conventional boiler when its furnace volume is changed to raise the combustion load to a level equal to that of this embodiment. In both cases, the same burner is used.
  • the combustion load of the conven­tional boiler is raised, the gas temperature in the furnace raises to increase the thermal NOx.
  • the broken line a representing the NOx concentration when the combustion load is increased is higher than the solid line A representing the NOx concentration when the combustion load is not increased. In brief, the NOx concentration is higher in the former at the same O2 concentration.
  • the gas residence time in the furnace becomes shorter and then the duration of contact between the gaseous fuel and the high-temperature gas also becomes shorter. Therefore, in regard to the concentration of unburnt contents, particularly of carbon monoxide, the broken line b representing CO concentration when the combustion load is increased is higher than the solid line B representing CO concentration when the combustion load is not increased. In brief, the CO concentration is higher when the combustion load is increased if the O2 concentration is the same.
  • the CO concentration in the exhuast gas is decreased as indicated by the dashed line C and therefore, the O2 concentration is low which is required to obtain the same CO concentration as the levels indicated by the solid line B and the broken line b .
  • the O2 concentration is set 0.3, the NOx concentration N3 becomes lower than the NOx concentration N1 of the conventional boiler under the same CO concen­tration, and than the NOx concentration N2 of the conventional boiler of high-load combustion, as well.
  • the provision of an unburnt gas combustor enables low-oxygen operation with O2 concentration lower than any other conventional boilers, and then reduces NOx.
  • the discharged quantity of carbon monoxide is increased by reduction of excess air to be supplied to the furnace.
  • Such carbon monoxide can be reduced by the unburnt gas combustor. Therefore, the furnace size can be reduced since it is unnecessary to increase the furnace size to restrain the quantity of carbon monoxide produced in the furnace.
  • the premixture throat 140 injects the premixture of an air ratio of 1 or less, preferably 0.5 to 0.9, in a swirl flow manner at 20 to 50 m/s into the primary combustion chamber 157.
  • the injected premixture is ignited by the pilot flame to form the main combustion flame. Since the air ratio of the premixture forming the main combustion flame is 1 or less, the thermal NOx produced by combustion is reduced through vapor-phase reduction by the combustion intermediate products of the gaseous fuel into nitrogen. Theus, the NOx concentration at the same O2 concentration is made lower than that shown by the broken line b in Fig. 19.
  • the main combustion flame is due to the premixture combustion and then has a combustion speed faster than the diffusion flame, the combustion velocity of which is controlled by mixing.
  • the primary combustion chamber 157 secures a combustion zone in which the main combustion flame is burnt at the air ratio of 1 or less. It prevents an unstable combustion of the pilot flame and the main combustion flame which is caused by combustion air from the combustion air passage 238.
  • the primary combustion chamber 157 is so designed that the ratio of l/d, i.e. the length l to the inner diameter d, is set 0.2 to 2, preferably 0.3 to 0.9.
  • the above-mentioned boiler is started up by supplying a predetermined quantity of air into the premix chamber 177 and a gaseous fuel to the fuel nozzle 152 to form a pilot flame under the air ratio to about 1.2, and thereafter by increasing the quantities of air and fuel to be supplied to the main premixture passage 212 while maintaining the air ratio of about 0.6, thereby setting the combustion load at a predeter­mined value.
  • the stability of the premixture flame can be improved by making it easy for the combustion of the premixture to progress from the central portion of the flow of the premixture by the action of a plate disposed downstream of the premixture injection outlet not parallel with the direction of the mainstream of the injected premixture.
  • NOx from the premixture flame can be greatly reduced at the excess air ratio of about 1.0 by mixing a part of the combustion gas into the mixture at the outer periphery of the mixture flow before the mixture starts to burn.
  • a premixture combustion system boiler according to the present invention, a high-load, low-NOx boiler can be realized because the quantity of NOx produced at the same excess air ratio does not change even when the combustion load is increased.
  • the boiler load can be changed stably from 10% to 100%.
  • a primary combustion chamber is provided in the burner, in which combustion chamber the combustion is effected with a low air ratio of 0.5 to 0.9.
  • the unburnt gas produced from the primary combustion chamber is burnt completely by residual oxygen from the secondary nozzle. In this manner, high-load, low-NOx combustion can be realized by a single burner.
  • a boiler according to the present invention burns the unburnt gas in the combustion gas in the middle of the exhaust gas duct, and therefore, the discharge of the unburnt gas can be greatly reduced. Thus, low-NOx combustion can be reduced.
EP89123973A 1988-12-26 1989-12-27 Kessel mit vermindertem NOx-Ausstoss Expired - Lifetime EP0376259B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP32584788A JPH0264302A (ja) 1988-05-02 1988-12-26 ボイラ及びそのバーナとその燃焼方法
JP325847/88 1988-12-26

Publications (3)

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EP0376259A2 true EP0376259A2 (de) 1990-07-04
EP0376259A3 EP0376259A3 (de) 1992-01-15
EP0376259B1 EP0376259B1 (de) 1996-05-22

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US (1) US5067419A (de)
EP (1) EP0376259B1 (de)
CN (1) CN1017744B (de)
DE (1) DE68926535T2 (de)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1995029365A1 (en) * 1994-04-26 1995-11-02 Radian Corporation APPARATUS AND METHOD FOR REDUCING NOx, CO AND HYDROCARBON EMISSIONS WHEN BURNING GASEOUS FUELS
EP0797051A2 (de) * 1996-03-20 1997-09-24 Abb Research Ltd. Brenner für einen Wärmeerzeuger
EP0909921A1 (de) * 1997-10-14 1999-04-21 Abb Research Ltd. Brenner für den Betrieb eines Wärmeerzeugers
US8925323B2 (en) 2012-04-30 2015-01-06 General Electric Company Fuel/air premixing system for turbine engine

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5417564A (en) * 1994-01-27 1995-05-23 Riley Stoker Corporation Method and apparatus for altering the firing pattern of an existing furnace
US5617716A (en) * 1994-09-16 1997-04-08 Electric Power Research Institute Method for supplying vaporized fuel oil to a gas turbine combustor and system for same
US5525053A (en) * 1994-12-01 1996-06-11 Wartsila Diesel, Inc. Method of operating a combined cycle power plant
US6837702B1 (en) 1994-12-01 2005-01-04 Wartsila Diesel, Inc. Method of operating a combined cycle power plant
US5690039A (en) * 1996-06-17 1997-11-25 Rjm Corporation Method and apparatus for reducing nitrogen oxides using spatially selective cooling
US6062848A (en) * 1998-05-29 2000-05-16 Coen Company, Inc. Vibration-resistant low NOx burner
GB2365117B (en) * 2000-07-28 2005-02-16 Planer Products Ltd Method of and apparatus for heating a substrate
AUPR229200A0 (en) * 2000-12-22 2001-01-25 Renewable Energy Corporation Limited Refractory wall structure and damper device
JP2004125380A (ja) * 2002-07-29 2004-04-22 Miura Co Ltd 低ＮＯｘ燃焼装置
US6979430B2 (en) * 2002-12-18 2005-12-27 Foster Wheeler Energy Corporation System and method for controlling NOx emissions from boilers combusting carbonaceous fuels without using external reagent
US8769960B2 (en) * 2005-10-21 2014-07-08 Rolls-Royce Canada, Ltd Gas turbine engine mixing duct and method to start the engine
KR20090057298A (ko) * 2006-09-11 2009-06-04 우드사이드 에너지 리미티드 Ｌｎｇ의 선박 대 선박 이송과정 중의 액체기화가스 처리
CN100453906C (zh) * 2006-11-23 2009-01-21 中国船舶重工集团公司第七一一研究所 蒸汽助燃型火炬燃烧器
US20080145805A1 (en) * 2006-12-14 2008-06-19 Towler Gavin P Process of Using a Fired Heater
US20100021853A1 (en) * 2008-07-25 2010-01-28 John Zink Company, Llc Burner Apparatus And Methods
US9404650B2 (en) * 2009-06-30 2016-08-02 M. Alexandre Lapierre Boiler with improved hot gas passages
US8545213B2 (en) * 2010-03-09 2013-10-01 Air Products And Chemicals, Inc. Reformer and method of operating the reformer
CN102853416B (zh) * 2011-06-27 2016-06-29 朱永彪 气体燃烧室
US10281140B2 (en) 2014-07-15 2019-05-07 Chevron U.S.A. Inc. Low NOx combustion method and apparatus
US10375901B2 (en) 2014-12-09 2019-08-13 Mtd Products Inc Blower/vacuum
IT201700106691A1 (it) * 2017-09-25 2019-03-25 I C I Caldaie S P A Caldaia.
JP2020098069A (ja) * 2018-12-18 2020-06-25 三浦工業株式会社 ボイラ及びボイラの制御方法
JP7260154B2 (ja) * 2019-05-27 2023-04-18 株式会社下瀬微生物研究所 ボイラー装置及びこれを備えた有機性廃棄物の処理装置
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Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1011058A (en) * 1962-04-05 1965-11-24 Fuel Firing Ltd Multi-stage burner unit
FR2167747A1 (de) * 1971-11-15 1973-08-24 Aqua Chem Inc
FR2219384A1 (de) * 1973-02-24 1974-09-20 Mitsubishi Heavy Ind Ltd
DE2428622A1 (de) * 1973-06-15 1975-01-09 O F R Officine Fratelli Riello Brennerkopf, insbesondere fuer gasfoermige brennstoffe
FR2263460A1 (de) * 1974-03-05 1975-10-03 Mitsubishi Heavy Ind Ltd
DE2534841A1 (de) * 1974-12-11 1976-06-24 Energiagazdalkodasi Intezet Feuerungsverfahren und feuerungsanlage
US4150539A (en) * 1976-02-05 1979-04-24 Avco Corporation Low pollution combustor
DE3222347A1 (de) * 1981-06-15 1983-01-20 Hitachi, Ltd., Tokyo Schwingbrenner mit vormischung
WO1986001876A1 (en) * 1984-09-12 1986-03-27 Air (Anti Pollution Industrial Research) Ltd. Method and apparatus for conducting a substantially isothermal combustion process in a combustor
GB2176588A (en) * 1985-06-13 1986-12-31 British Gas Corp Gas burner
DE3702415C1 (de) * 1987-01-28 1988-04-21 Babcock Werke Ag Brenner
DE3707773A1 (de) * 1987-03-11 1988-09-22 Bbc Brown Boveri & Cie Verfahren und einrichtung zur prozesswaermeerzeugung

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3894834A (en) * 1973-10-17 1975-07-15 Airco Inc Ignition and flame stabilization system for coal-air furnace
US3940253A (en) * 1973-12-07 1976-02-24 Volvo Flygmotor Aktiebolag Device for the purification of process waste gases
US4368677A (en) * 1981-04-07 1983-01-18 Kline Michael J Pulse combustion system for boilers
JP2526236B2 (ja) * 1987-02-27 1996-08-21 バブコツク日立株式会社 超低ＮＯｘ燃焼装置
US4951579A (en) * 1987-11-18 1990-08-28 Radian Corporation Low NOX combustion process
FR2625295B1 (fr) * 1987-12-24 1990-04-13 Gaz De France Procede et appareil destines a assurer la combustion etagee d'un melange combustible-comburant diminuant la production d'oxydes d'azote

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1011058A (en) * 1962-04-05 1965-11-24 Fuel Firing Ltd Multi-stage burner unit
FR2167747A1 (de) * 1971-11-15 1973-08-24 Aqua Chem Inc
US3816595A (en) * 1971-11-15 1974-06-11 Aqua Chem Inc Method and apparatus for removing nitrogen oxides from a gas stream
FR2219384A1 (de) * 1973-02-24 1974-09-20 Mitsubishi Heavy Ind Ltd
DE2428622A1 (de) * 1973-06-15 1975-01-09 O F R Officine Fratelli Riello Brennerkopf, insbesondere fuer gasfoermige brennstoffe
FR2263460A1 (de) * 1974-03-05 1975-10-03 Mitsubishi Heavy Ind Ltd
DE2534841A1 (de) * 1974-12-11 1976-06-24 Energiagazdalkodasi Intezet Feuerungsverfahren und feuerungsanlage
US4150539A (en) * 1976-02-05 1979-04-24 Avco Corporation Low pollution combustor
DE3222347A1 (de) * 1981-06-15 1983-01-20 Hitachi, Ltd., Tokyo Schwingbrenner mit vormischung
WO1986001876A1 (en) * 1984-09-12 1986-03-27 Air (Anti Pollution Industrial Research) Ltd. Method and apparatus for conducting a substantially isothermal combustion process in a combustor
GB2176588A (en) * 1985-06-13 1986-12-31 British Gas Corp Gas burner
DE3702415C1 (de) * 1987-01-28 1988-04-21 Babcock Werke Ag Brenner
DE3707773A1 (de) * 1987-03-11 1988-09-22 Bbc Brown Boveri & Cie Verfahren und einrichtung zur prozesswaermeerzeugung

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
PROGRESS IN ENERGY AND COMBUSTION SCIENCE, vol. 6, no. 4, 1980, pages 303-329, Oxford, GB; C.J. RALLIS et al.: "The determination of laminar burning velocity"; Page 310, right-hand column, last paragraph; page 311, left-hand column, paragraph 1; page 312, figure 11. *

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1995029365A1 (en) * 1994-04-26 1995-11-02 Radian Corporation APPARATUS AND METHOD FOR REDUCING NOx, CO AND HYDROCARBON EMISSIONS WHEN BURNING GASEOUS FUELS
EP0797051A2 (de) * 1996-03-20 1997-09-24 Abb Research Ltd. Brenner für einen Wärmeerzeuger
EP0797051A3 (de) * 1996-03-20 1998-05-20 Abb Research Ltd. Brenner für einen Wärmeerzeuger
EP0909921A1 (de) * 1997-10-14 1999-04-21 Abb Research Ltd. Brenner für den Betrieb eines Wärmeerzeugers
US5954495A (en) * 1997-10-14 1999-09-21 Abb Research Ltd. Burner for operating a heat generator
US8925323B2 (en) 2012-04-30 2015-01-06 General Electric Company Fuel/air premixing system for turbine engine

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CN1017744B (zh) 1992-08-05
DE68926535D1 (de) 1996-06-27
EP0376259A3 (de) 1992-01-15
US5067419A (en) 1991-11-26
DE68926535T2 (de) 1996-10-17
CN1044979A (zh) 1990-08-29
EP0376259B1 (de) 1996-05-22

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